Credit
Rijkswaterstaat · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
402C Businessliner · Length
Single source36 ft 4 + 1 ⁄ 2 in (11.09 m)[source]
Falcon 20F · Length
Configuration
| Specification | Cessna 402 | Dassault Falcon 20 |
|---|---|---|
| Type | Corporate transport and airliner[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Status | In service[source] | Out of production, in active service |
17.15 m (56 ft 3 in)[source]
Empty; 402C Businessliner · Empty weight
Single sourceMaximum take-off; 402C Businessliner · Max takeoff weight
Single source4,077 lb (1,849 kg)[source]
6,850 lb (3,107 kg)[source]
Empty; Falcon 20F · Empty weight
Single sourceMaximum take-off; Falcon 20F · Max takeoff weight
Single sourceCruise; 402C Businessliner · at 10,000 ft (3,000 m) (econ cruise)
Single sourceMaximum; 402C Businessliner · at 16,000 ft (4,900 m)
Single source231 kn (266 mph, 428 km/h) at 16,000 ft (4,900 m)[source]
142 kn (163 mph, 263 km/h) at 10,000 ft (3,000 m) (econ cruise)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source402C Businessliner · 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines each
Single source2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 kW) each[source]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
402C Businessliner · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Cape Air[source] | — |
|---|
| Number built | 2,000+[source] | 512[source] |
|---|
| Manufactured | 1966–1985[source] | 1965–1991[source] |
|---|
| Introduction date | 1967[source] | 3 June 1965[source] |
|---|
| First flight | August 26, 1965[source] | 4 May 1963[source] |
|---|
| Developed from | Cessna 411[source] | — |
|---|
| Developed into | Cessna 404 Titan Cessna 414[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | Six passengers[source] | 8–14 passengers[source] |
|---|
| Airfoil | NACA 23018 (root) NACA 23015 (tip)[source] | — |
|---|
| Fuel capacity | 206 US gal (172 imp gal; 780 L) usable fuel[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Propellers | 3-bladed McCauley 0850334-34 constant speed propeller[source] | — |
|---|
| Stall speed | 68 kn (78 mph, 126 km/h) (flaps down, power off) (CAS)[source] | 152 km/h (94 mph, 82 kn)[source] |
|---|
| Never exceed speed | 231 kn (266 mph, 428 km/h) ( CAS )[source] | — |
|---|
| Takeoff distance to 50 ft (15m) | 2,195 ft (669 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 2,485 ft (757 m)[source] | — |
|---|
| Primary users | — | Federal Express (formerly) French Navy United States Coast Guard[source] |
|---|
| Aspect ratio | — | 6.4:1[source] |
|---|